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  • Attitude dynamics of a compound solar sail

    Paper number

    IAC-06-C1.1.08

    Author

    Dr. Anna Guerman, University of Beira Interior, Portugal

    Coauthor

    Prof. Georgi Smirnov, University of Porto, Portugal

    Year

    2006

    Abstract

    The use of solar pressure to create propulsion can minimize on-board energy consumption during a mission. Many projects of solar sails are now under development, making solar sail dynamics the subject of numerous studies.

    So far, the most extensively studied problem is the orbital maneuver of a Flat Solar Sail (FSS). In this case, the control is performed by turning the entire sail surface with respect to the sun-sailcraft direction. This changes the radiation pressure and results in evolution of the vehicle trajectory.

    The use of Solar Photon Thruster (SPT) was proposed long ago [1], but the study of this spacecraft began quite recently. The SPT consists of a parabolic surface which concentrates the solar radiation pressure on a system of smaller mirrors. The control effort in such system is produced by displacement of a small mirror with respect to the parabolic surface. The sail axis is supposed to be oriented along the sun-sailcraft direction.

    In the present article, we examine attitude motion and stabilization of a parabolic compound sailcraft. We study two versions of the SPT scheme, Dual Reflector SPT (DR SPT) that includes a collimator and the Simple SPT (SSPT). Both schemes are described in [1]. Here we compare the feasibility of these two schemes.

    Equations of orbital motion for ideal DR SPT were deduced in [1] and used in several studies to investigate trajectory control of this sailcraft. In [2] we developed a force-torque model for the SSPT supposing its ideal reflection properties, and compared it with an ideal FSS. Now we deduce the equations of trajectory and attitude motion for a non-ideal SPT sailcraft. We study its orbital behavior and the corresponding attitude dynamics. We analyze the possibility of SPT attitude stabilization.

    [1] R.L. Forward, Solar photon thruster, J. Spacecraft, 27(4), 1990, 411- 416.

    [2] A.D. Guerman, and G. Smirnov, Attitude Control of Solar Photon Thruster vs Plane Solar Sail, Advances in the Astronautical Sciences, 2006, 123, 2635 - 2648.

    Abstract document

    IAC-06-C1.1.08.pdf

    Manuscript document

    IAC-06-C1.1.08.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.